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booz2_g1.xml
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booz2_g1.xml
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<airframe name="BOOZ2_G1">
<modules main_freq="512">
<!--load name="booz_pwm.xml"/-->
<!--load name="booz_drop.xml"/-->
<!--load name="booz_cam.xml"/-->
<!--load name="sonar_maxbotix_booz.xml"/-->
<!--load name="adc_generic_booz.xml"/-->
<!--load name="sys_mon.xml"/-->
</modules>
<firmware name="rotorcraft">
<define name="USE_INS_NAV_INIT"/>
<define name="USE_ADAPT_HOVER"/>
<define name="NO_FUCKING_STARTUP_DELAY"/>
<!--define name="GUIDANCE_H_USE_REF"/-->
<target name="ap" board="booz_1.0">
<define name="FAILSAFE_GROUND_DETECT"/>
<define name="USE_GPS_ACC4R"/>
<define name="BOOZ_START_DELAY" value="3"/>
</target>
<target name="sim" board="pc">
<subsystem name="fdm" type="nps"/>
<!--define name="NPS_NO_SUPERVISION"/-->
</target>
<subsystem name="radio_control" type="ppm"/>
<subsystem name="telemetry" type="transparent"/>
<subsystem name="actuators" type="asctec"/>
<subsystem name="imu" type="b2_v1.1"/>
<subsystem name="gps" type="ublox">
<configure name="GPS_BAUD" value="B57600"/>
</subsystem>
<subsystem name="ahrs" type="cmpl"/>
<subsystem name="ins" type="hff"/>
</firmware>
<firmware name="booz_test_progs">
<target name="test_telemetry" board="booz_1.0"/>
<target name="test_baro" board="booz_1.0"/>
<target name="test_rc_spektrum" board="booz_1.0"/>
<target name="test_rc_ppm" board="booz_1.0"/>
</firmware>
<servos min="0" neutral="0" max="0xff">
<servo name="PITCH" no="0" min="0" neutral="0" max="255"/>
<servo name="ROLL" no="1" min="0" neutral="0" max="255"/>
<servo name="YAW" no="2" min="0" neutral="0" max="255"/>
<servo name="THRUST" no="3" min="0" neutral="0" max="255"/>
</servos>
<commands>
<axis name="PITCH" failsafe_value="0"/>
<axis name="ROLL" failsafe_value="0"/>
<axis name="YAW" failsafe_value="0"/>
<axis name="THRUST" failsafe_value="0"/>
</commands>
<section name="SUPERVISION" prefix="SUPERVISION_">
<define name="TRIM_A" value="0"/>
<define name="TRIM_E" value="6"/>
<define name="TRIM_R" value="0"/>
</section>
<section name="IMU" prefix="IMU_">
<define name="GYRO_P_NEUTRAL" value="32238"/>
<define name="GYRO_Q_NEUTRAL" value="32391"/>
<define name="GYRO_R_NEUTRAL" value="32853"/>
<define name="GYRO_P_SENS" value="1.00" integer="16"/>
<define name="GYRO_Q_SENS" value="1.00" integer="16"/>
<define name="GYRO_R_SENS" value="1.00" integer="16"/>
<define name="ACCEL_X_SENS" value="2.55975587" integer="16"/>
<define name="ACCEL_Y_SENS" value="2.55643340" integer="16"/>
<define name="ACCEL_Z_SENS" value="2.57178460" integer="16"/>
<define name="ACCEL_X_NEUTRAL" value="33067"/>
<define name="ACCEL_Y_NEUTRAL" value="32778"/>
<define name="ACCEL_Z_NEUTRAL" value="32140"/>
<define name="MAG_X_NEUTRAL" value="-12"/>
<define name="MAG_Y_NEUTRAL" value="-10"/>
<define name="MAG_Z_NEUTRAL" value="-11"/>
<define name="MAG_X_SENS" value="22.008352" integer="16"/>
<define name="MAG_Y_SENS" value="21.79885" integer="16"/>
<define name="MAG_Z_SENS" value="14.675745" integer="16"/>
<define name="BODY_TO_IMU_PHI" value="RadOfDeg(1.3)"/>
<define name="BODY_TO_IMU_THETA" value="RadOfDeg(-2.6)"/>
<define name="BODY_TO_IMU_PSI" value="RadOfDeg(0.)"/>
</section>
<section name="STABILIZATION_RATE" prefix="STABILIZATION_RATE_">
<define name="SP_MAX_P" value="10000"/>
<define name="SP_MAX_Q" value="10000"/>
<define name="SP_MAX_R" value="10000"/>
<define name="GAIN_P" value="-400"/>
<define name="GAIN_Q" value="-400"/>
<define name="GAIN_R" value="-350"/>
</section>
<section name="STABILIZATION_ATTITUDE" prefix="STABILIZATION_ATTITUDE_">
<!-- setpoints -->
<define name="SP_MAX_PHI" value="RadOfDeg(45.)"/>
<define name="SP_MAX_THETA" value="RadOfDeg(45.)"/>
<define name="SP_MAX_R" value="RadOfDeg(90.)"/>
<define name="DEADBAND_R" value="250"/>
<!-- reference -->
<define name="REF_OMEGA_P" value="RadOfDeg(800)"/>
<define name="REF_ZETA_P" value="0.85"/>
<define name="REF_MAX_P" value="RadOfDeg(300.)"/>
<define name="REF_MAX_PDOT" value="RadOfDeg(7000.)"/>
<define name="REF_OMEGA_Q" value="RadOfDeg(800)"/>
<define name="REF_ZETA_Q" value="0.85"/>
<define name="REF_MAX_Q" value="RadOfDeg(300.)"/>
<define name="REF_MAX_QDOT" value="RadOfDeg(7000.)"/>
<define name="REF_OMEGA_R" value="RadOfDeg(500)"/>
<define name="REF_ZETA_R" value="0.85"/>
<define name="REF_MAX_R" value="RadOfDeg(90.)"/>
<define name="REF_MAX_RDOT" value="RadOfDeg(900.)"/>
<!-- feedback -->
<define name="PHI_PGAIN" value="-2000"/>
<define name="PHI_DGAIN" value="-400"/>
<define name="PHI_IGAIN" value="-200"/>
<define name="THETA_PGAIN" value="-2000"/>
<define name="THETA_DGAIN" value="-400"/>
<define name="THETA_IGAIN" value="-200"/>
<define name="PSI_PGAIN" value="-2000"/>
<define name="PSI_DGAIN" value="-400"/>
<define name="PSI_IGAIN" value="-10"/>
<!-- feedforward -->
<define name="PHI_DDGAIN" value=" 300"/>
<define name="THETA_DDGAIN" value=" 300"/>
<define name="PSI_DDGAIN" value=" 300"/>
</section>
<section name="INS" prefix="INS_">
<define name="BARO_SENS" value="15." integer="16"/>
<define name="UNTILT_ACCEL" value="1"/>
<define name="SONAR_SENS" value="2.146" integer="16"/>
</section>
<section name="GUIDANCE_V" prefix="GUIDANCE_V_">
<define name="MIN_ERR_Z" value="POS_BFP_OF_REAL(-10.)"/>
<define name="MAX_ERR_Z" value="POS_BFP_OF_REAL( 10.)"/>
<define name="MIN_ERR_ZD" value="SPEED_BFP_OF_REAL(-10.)"/>
<define name="MAX_ERR_ZD" value="SPEED_BFP_OF_REAL( 10.)"/>
<define name="MAX_SUM_ERR" value="2000000"/>
<define name="REF_MIN_ZDD" value="-1.5*9.81"/>
<define name="REF_MAX_ZDD" value=" 0.5*9.81"/>
<define name="REF_MIN_ZD" value="-1.5"/>
<define name="REF_MAX_ZD" value=" 1.5"/>
<define name="HOVER_KP" value="-150"/>
<define name="HOVER_KD" value="-80"/>
<define name="HOVER_KI" value="0"/>
<!-- 1.5m/s for full stick : SPEED_BFP_OF_REAL(1.5) / (MAX_PPRZ/2) -->
<define name="RC_CLIMB_COEF" value ="163"/>
<!-- SPEED_BFP_OF_REAL(1.5) * 20% -->
<define name="RC_CLIMB_DEAD_BAND" value ="160000"/>
<!-- <define name="INV_M" value="0.118"/> -->
</section>
<section name="GUIDANCE_H" prefix="GUIDANCE_H_">
<define name="PGAIN" value="-50"/>
<define name="DGAIN" value="-100"/>
<define name="IGAIN" value="-15"/>
<define name="NGAIN" value="-0"/>
<!-- feedforward -->
<define name="AGAIN" value="100"/>
</section>
<section name="BAT">
<define name="MILLIAMP_PER_PERCENT" value="0.86"/>
<define name="CATASTROPHIC_BAT_LEVEL" value="9.3" unit="V"/>
<define name="BATTERY_SENS" value="0.183" integer="16"/>
</section>
<section name="AUTOPILOT">
<define name="MODE_MANUAL" value="AP_MODE_ATTITUDE_DIRECT"/>
<define name="MODE_AUTO1" value="AP_MODE_ATTITUDE_Z_HOLD"/>
<define name="MODE_AUTO2" value="AP_MODE_NAV"/>
</section>
<section name="FMS">
<define name="BOOZ_FMS_TIMEOUT" value="0"/>
</section>
<section name="CAM" prefix="BOOZ_CAM_">
<define name="TILT_NEUTRAL" value="1500"/>
<define name="TILT_MIN" value="1000"/>
<define name="TILT_MAX" value="2000"/>
<define name="TILT_ANGLE_MIN" value="RadOfDeg(-85.)" unit="rad"/>
<define name="TILT_ANGLE_MAX" value="RadOfDeg( 30.)" unit="rad"/>
<define name="PAN_NEUTRAL" value="0"/>
<define name="PAN_MIN" value="0"/>
<define name="PAN_MAX" value="25736"/> <!-- 360 deg (2^12) -->
</section>
<section name="MISC">
<define name="BOOZ_ANALOG_BARO_THRESHOLD" value="800"/>
<define name="FACE_REINJ_1" value="1024"/>
<define name="DEFAULT_CIRCLE_RADIUS" value="10."/>
</section>
<section name="GCS">
<define name="ALT_SHIFT_PLUS_PLUS" value="5"/>
<define name="ALT_SHIFT_PLUS" value="1"/>
<define name="ALT_SHIFT_MINUS" value="-1"/>
</section>
<section name="SIMULATOR" prefix="NPS_">
<define name="ACTUATOR_NAMES" value="{"front_motor", "back_motor", "right_motor", "left_motor"}"/>
<!--define name="INITIAL_CONDITITONS" value=""reset_enac""/-->
<define name="SENSORS_PARAMS" value=""nps_sensors_params_booz2_a1.h""/>
</section>
</airframe>